EA201691308A1 - MANAGEMENT OF SPATIAL POSITION FOR MANOVE SATELLITE DEVICES - Google Patents

MANAGEMENT OF SPATIAL POSITION FOR MANOVE SATELLITE DEVICES

Info

Publication number
EA201691308A1
EA201691308A1 EA201691308A EA201691308A EA201691308A1 EA 201691308 A1 EA201691308 A1 EA 201691308A1 EA 201691308 A EA201691308 A EA 201691308A EA 201691308 A EA201691308 A EA 201691308A EA 201691308 A1 EA201691308 A1 EA 201691308A1
Authority
EA
Eurasian Patent Office
Prior art keywords
spatial position
management
manove
present
satellite devices
Prior art date
Application number
EA201691308A
Other languages
Russian (ru)
Inventor
Марко Анания
Доменико Касконе
Original Assignee
Таль Аления Спейс Италия С.П.А. Кон Унико Сочио
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Таль Аления Спейс Италия С.П.А. Кон Унико Сочио filed Critical Таль Аления Спейс Италия С.П.А. Кон Унико Сочио
Publication of EA201691308A1 publication Critical patent/EA201691308A1/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/286—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using control momentum gyroscopes (CMGs)
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/244—Spacecraft control systems
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/02—Rotary gyroscopes
    • G01C19/04—Details
    • G01C19/06—Rotors
    • G01C19/065—Means for measuring or controlling of rotors' angular velocity
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
    • F16M2200/00—Details of stands or supports
    • F16M2200/06—Arms
    • F16M2200/065—Arms with a special structure, e.g. reinforced or adapted for space reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Astronomy & Astrophysics (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

Настоящее изобретение относится, в общем, к управлению пространственным положением и, в частности, к управлению пространственным положением космической платформы, в частности спутника и/или космического летательного аппарата. Подробно, аспект настоящего изобретения касается использования, в системе (100) управления пространственным положением, нескольких моментных управляющих гироскопов (3, 41, 42, 43, 44, 61, 62, 63, 64) с ограниченным числом оборотов подвеса гироскопа. Кроме того, другой аспект настоящего изобретения касается улучшенной логики для управления моментным управляющим гироскопным узлом (4, 6, 120) системы (100) управления пространственным положением.The present invention relates, in general, to the management of the spatial position and, in particular, to the management of the spatial position of the space platform, in particular the satellite and / or the spacecraft. In detail, an aspect of the present invention concerns the use, in the system for managing the spatial position, of several torque control gyros (3, 41, 42, 43, 44, 61, 62, 63, 64) with a limited number of revolutions of the gyroscope. In addition, another aspect of the present invention relates to improved logic for controlling a torque controlling gyro unit (4, 6, 120) of the attitude control system (100).

EA201691308A 2013-12-23 2014-12-23 MANAGEMENT OF SPATIAL POSITION FOR MANOVE SATELLITE DEVICES EA201691308A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
IT001067A ITTO20131067A1 (en) 2013-12-23 2013-12-23 TRIMMING CONTROL SYSTEM FOR AGILE SATELLITE APPLICATIONS
PCT/IB2014/067282 WO2015097672A2 (en) 2013-12-23 2014-12-23 Attitude control for agile satellite applications

Publications (1)

Publication Number Publication Date
EA201691308A1 true EA201691308A1 (en) 2016-11-30

Family

ID=50116102

Family Applications (2)

Application Number Title Priority Date Filing Date
EA201891068A EA201891068A1 (en) 2013-12-23 2014-12-23 MANAGEMENT OF SPATIAL POSITION FOR MANOVE SATELLITE DEVICES
EA201691308A EA201691308A1 (en) 2013-12-23 2014-12-23 MANAGEMENT OF SPATIAL POSITION FOR MANOVE SATELLITE DEVICES

Family Applications Before (1)

Application Number Title Priority Date Filing Date
EA201891068A EA201891068A1 (en) 2013-12-23 2014-12-23 MANAGEMENT OF SPATIAL POSITION FOR MANOVE SATELLITE DEVICES

Country Status (13)

Country Link
US (2) US10703511B2 (en)
EP (2) EP3087006B1 (en)
KR (1) KR102266872B1 (en)
CN (2) CN106068440B (en)
AU (2) AU2014372139B2 (en)
BR (1) BR112016014819A2 (en)
EA (2) EA201891068A1 (en)
ES (1) ES2694691T3 (en)
IT (1) ITTO20131067A1 (en)
MX (1) MX2016008286A (en)
PL (1) PL3087006T3 (en)
SG (2) SG11201604913TA (en)
WO (1) WO2015097672A2 (en)

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ITTO20131067A1 (en) * 2013-12-23 2015-06-24 Thales Alenia Space Italia S P A C On Unico Socio TRIMMING CONTROL SYSTEM FOR AGILE SATELLITE APPLICATIONS
US11221633B2 (en) * 2016-05-17 2022-01-11 Raytheon Company Gyroscopic attitude control system
CN107089348B (en) * 2017-04-01 2019-04-30 中国空间技术研究院 On-orbit fault game method based on more flexible accessory satellite dynamics optimized Control Modes
US10276997B1 (en) 2017-10-06 2019-04-30 Honeywell International Inc. Wire assembly including clockspring passes
CN109828595A (en) * 2019-01-31 2019-05-31 中国人民解放军国防科技大学 Method for analyzing approaching feasibility of terminal of dead space spacecraft
CN110329548B (en) * 2019-05-24 2023-01-17 中国人民解放军63789部队 Flywheel system reconstruction method under on-orbit rotation bias control of spacecraft
CN110658838B (en) * 2019-09-19 2022-10-28 北京控制工程研究所 Method and system for calculating three-axis maneuvering angular velocity of agile spacecraft in real time
CN110658837B (en) * 2019-09-19 2020-10-23 北京控制工程研究所 Steady reconstruction method under control moment gyro fault condition
CN111897355B (en) * 2020-08-06 2022-09-13 中国科学院微小卫星创新研究院 Satellite attitude maneuver trajectory planning method
CN112061425B (en) * 2020-09-08 2022-04-08 上海航天控制技术研究所 Method for avoiding interference of earth gas light on agile small satellite star sensor
CN114313311B (en) * 2022-03-04 2022-05-27 中国人民解放军战略支援部队航天工程大学 Topological structure of multi-body allosteric satellite
CN117330049B (en) * 2023-11-27 2024-01-30 中北大学 Cavity internal reflection high-robustness angular velocity sensor based on singular surface and measuring method

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US7805226B2 (en) * 2006-09-29 2010-09-28 Honeywell International Inc. Hierarchical strategy for singularity avoidance in arrays of control moment gyroscopes
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US20110011982A1 (en) * 2009-07-20 2011-01-20 Jason Herman Modular control moment gyroscope (cmg) system for spacecraft attitude control
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Also Published As

Publication number Publication date
EP3087006B1 (en) 2018-08-29
CN110329550A (en) 2019-10-15
CN110329550B (en) 2022-09-06
CN106068440A (en) 2016-11-02
ITTO20131067A1 (en) 2015-06-24
PL3087006T3 (en) 2019-01-31
EA201891068A1 (en) 2019-03-29
SG10201805372WA (en) 2018-08-30
CN106068440B (en) 2019-08-09
KR20160125357A (en) 2016-10-31
AU2018200772A1 (en) 2018-02-22
WO2015097672A3 (en) 2015-10-29
WO2015097672A2 (en) 2015-07-02
SG11201604913TA (en) 2016-07-28
US10703511B2 (en) 2020-07-07
AU2014372139A1 (en) 2016-07-07
EP3216705B1 (en) 2019-01-30
EP3087006A2 (en) 2016-11-02
KR102266872B1 (en) 2021-06-21
ES2694691T3 (en) 2018-12-26
US20170029139A1 (en) 2017-02-02
US20200047922A1 (en) 2020-02-13
MX2016008286A (en) 2017-01-09
AU2014372139B2 (en) 2018-02-22
BR112016014819A2 (en) 2017-08-08
EP3216705A1 (en) 2017-09-13

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